View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 65230U 26145.60203163 +.00000000 +00000-0 +14307-3 0 00006
2 65230 86.4960 21.0196 0001663 88.6308 271.5016 13.24412581 02
| Epoch (UTC): | 25 May 2026 14:26:55 |
| Eccentricity: | 0.0001663 |
| inclination: | 86.4960° |
| perigee height: | 1167 km |
| apogee height: | 1169 km |
| right ascension of ascending node: | 21.0196° |
| argument of perigee: | 88.6308° |
| revolutions per day: | 13.24412581 |
| mean anomaly at epoch: | 271.5016° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|